NASA NTRS ยท 19720045919
Sonic-boom calculation in a stratified atmosphere.
Abstract
For a lifting body of revolution, the exact solutions to the gas dynamical equation are given for the flow field in a stratified atmosphere. The boundary condition is satisfied by using the (linearized) slender-body theory. The solution allows one to make a prediction of the magnitude and the location of the sonic boom in a stratified atmosphere as well as to handle cutoff effects.
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Schorling, M.. 1972-01-01. Sonic-boom calculation in a stratified atmosphere.. https://ntrs.nasa.gov/citations/19720045919
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